CN115867521B - 由陶瓷基复合材料制造喷嘴叶片的方法 - Google Patents
由陶瓷基复合材料制造喷嘴叶片的方法 Download PDFInfo
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- CN115867521B CN115867521B CN202180047859.6A CN202180047859A CN115867521B CN 115867521 B CN115867521 B CN 115867521B CN 202180047859 A CN202180047859 A CN 202180047859A CN 115867521 B CN115867521 B CN 115867521B
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- Prior art keywords
- preform
- central portion
- blade
- fibrous
- hollow central
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- 238000004519 manufacturing process Methods 0.000 title claims abstract description 11
- 239000011153 ceramic matrix composite Substances 0.000 title claims abstract description 6
- 239000000835 fiber Substances 0.000 claims description 54
- 238000000034 method Methods 0.000 claims description 23
- 239000011159 matrix material Substances 0.000 claims description 14
- 238000000926 separation method Methods 0.000 claims description 12
- 230000002787 reinforcement Effects 0.000 claims description 11
- 239000000463 material Substances 0.000 claims description 9
- 239000000919 ceramic Substances 0.000 claims description 7
- 238000009954 braiding Methods 0.000 claims description 5
- 239000007788 liquid Substances 0.000 claims description 5
- 238000009941 weaving Methods 0.000 claims description 4
- 238000001564 chemical vapour infiltration Methods 0.000 claims 1
- 238000001764 infiltration Methods 0.000 description 4
- 230000008595 infiltration Effects 0.000 description 4
- 238000001816 cooling Methods 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 238000000626 liquid-phase infiltration Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 238000000197 pyrolysis Methods 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Classifications
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- C—CHEMISTRY; METALLURGY
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- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/001—Joining burned ceramic articles with other burned ceramic articles or other articles by heating directly with other burned ceramic articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
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- B32B18/00—Layered products essentially comprising ceramics, e.g. refractory products
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
- B32B3/06—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions for securing layers together; for attaching the product to another member, e.g. to a support, or to another product, e.g. groove/tongue, interlocking
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- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
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- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
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- F01D5/284—Selection of ceramic materials
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
- F01D9/044—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators permanently, e.g. by welding, brazing, casting or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/14—Making preforms characterised by structure or composition
- B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2250/00—Layers arrangement
- B32B2250/02—2 layers
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- B32B37/0038—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding involving application of liquid to the layers prior to lamination, e.g. wet laminating
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- C04B2235/524—Non-oxidic, e.g. borides, carbides, silicides or nitrides
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- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/60—Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
- C04B2235/616—Liquid infiltration of green bodies or pre-forms
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- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/38—Fiber or whisker reinforced
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- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/84—Joining of a first substrate with a second substrate at least partially inside the first substrate, where the bonding area is at the inside of the first substrate, e.g. one tube inside another tube
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Structural Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Textile Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
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FRFR2007063 | 2020-07-03 | ||
FR2007063A FR3112142B1 (fr) | 2020-07-03 | 2020-07-03 | Procédé de fabrication d’une aube de distributeur en matériau composite à matrice céramique |
PCT/FR2021/051148 WO2022003276A1 (fr) | 2020-07-03 | 2021-06-23 | Procédé de fabrication d'une aube de distributeur en matériau composite à matrice céramique |
Publications (2)
Publication Number | Publication Date |
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CN115867521A CN115867521A (zh) | 2023-03-28 |
CN115867521B true CN115867521B (zh) | 2024-03-29 |
Family
ID=75108355
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202180047859.6A Active CN115867521B (zh) | 2020-07-03 | 2021-06-23 | 由陶瓷基复合材料制造喷嘴叶片的方法 |
Country Status (5)
Country | Link |
---|---|
US (1) | US11772359B2 (fr) |
EP (1) | EP4175928B1 (fr) |
CN (1) | CN115867521B (fr) |
FR (1) | FR3112142B1 (fr) |
WO (1) | WO2022003276A1 (fr) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102387908A (zh) * | 2009-04-06 | 2012-03-21 | 斯奈克玛 | 一种用复合材料制成的涡轮机叶片的制造方法 |
CN103124606A (zh) * | 2010-09-28 | 2013-05-29 | 斯奈克玛 | 制造部件的方法及使用该方法获得的复合固体部件 |
CN103492724A (zh) * | 2010-07-02 | 2014-01-01 | 斯奈克玛 | 具有完整复合纵梁的叶片 |
CN103796818A (zh) * | 2011-09-07 | 2014-05-14 | 斯奈克玛 | 制造用于涡轮发动机的由复合材料所制造的涡轮机喷嘴或压气机定子叶片的扇体的方法,以及包括由所述扇体所组成喷嘴或定子叶片的涡轮机或压气机 |
CN107428103A (zh) * | 2015-02-16 | 2017-12-01 | 赛峰航空器发动机 | 用于制造由复合材料制成的涡轮机叶片的方法 |
CN111164061A (zh) * | 2017-10-02 | 2020-05-15 | 赛峰集团陶瓷 | 用于制造由陶瓷基复合材料制成的中空部件的方法 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2983519B1 (fr) * | 2011-12-01 | 2015-07-24 | Snecma Propulsion Solide | Aube de turbine a pale creuse en materiau composite, turbine ou compresseur ayant un distributeur ou redresseur forme de telles aubes et turbomachine les comprenant |
US10859268B2 (en) * | 2018-10-03 | 2020-12-08 | Rolls-Royce Plc | Ceramic matrix composite turbine vanes and vane ring assemblies |
US11035239B2 (en) * | 2018-10-25 | 2021-06-15 | General Electric Company | Ceramic matrix composite turbine nozzle shell and method of assembly |
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2020
- 2020-07-03 FR FR2007063A patent/FR3112142B1/fr active Active
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2021
- 2021-06-23 US US18/012,149 patent/US11772359B2/en active Active
- 2021-06-23 WO PCT/FR2021/051148 patent/WO2022003276A1/fr active Application Filing
- 2021-06-23 EP EP21740167.8A patent/EP4175928B1/fr active Active
- 2021-06-23 CN CN202180047859.6A patent/CN115867521B/zh active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
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CN102387908A (zh) * | 2009-04-06 | 2012-03-21 | 斯奈克玛 | 一种用复合材料制成的涡轮机叶片的制造方法 |
CN103492724A (zh) * | 2010-07-02 | 2014-01-01 | 斯奈克玛 | 具有完整复合纵梁的叶片 |
CN103124606A (zh) * | 2010-09-28 | 2013-05-29 | 斯奈克玛 | 制造部件的方法及使用该方法获得的复合固体部件 |
CN103796818A (zh) * | 2011-09-07 | 2014-05-14 | 斯奈克玛 | 制造用于涡轮发动机的由复合材料所制造的涡轮机喷嘴或压气机定子叶片的扇体的方法,以及包括由所述扇体所组成喷嘴或定子叶片的涡轮机或压气机 |
CN107428103A (zh) * | 2015-02-16 | 2017-12-01 | 赛峰航空器发动机 | 用于制造由复合材料制成的涡轮机叶片的方法 |
CN111164061A (zh) * | 2017-10-02 | 2020-05-15 | 赛峰集团陶瓷 | 用于制造由陶瓷基复合材料制成的中空部件的方法 |
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US11772359B2 (en) | 2023-10-03 |
EP4175928A1 (fr) | 2023-05-10 |
FR3112142B1 (fr) | 2022-09-09 |
CN115867521A (zh) | 2023-03-28 |
WO2022003276A1 (fr) | 2022-01-06 |
US20230191746A1 (en) | 2023-06-22 |
FR3112142A1 (fr) | 2022-01-07 |
EP4175928B1 (fr) | 2024-07-24 |
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